As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) A HIGHER THAN NORMAL T.O.T. WAS EXPERIENCED UNDER NORMAL OPERATING TO-QUE SETTINGS. AIRCRAFT ENGINE WAS INSPECTED UPON LANDING TO DETECT A POSSIBLE MALFUNCTION. A CRACK WAS DISCOVERED IN THE COMBUSTION CASE ASSEMBLY IN THE REINFORCED PATCH AREA OF THE LEFT TUBE INSIDE CURVE AREA. A PREVIOUS AND RECURRING PROBLEM; HENCE, THE REINFORCING PATCH.